AECMA PREN 2713-010-1995 Aerospace Series Cables Electrical Single and Multicore for General Purpose Operating Temperatures between - 55 Degrees C and 200 Degrees C Part 010 Scree.pdf

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1、 STDOAECMA PREN 2713-01O-ENGL 1775 L01231L 0012778 887 AECMA STANDARD NORME AECMA AECMA NORM prEN 27 13-01 O Edition P 1 March 1995 EDITE PAR LASSOCIATION EUROPCENNE DES CONSTRUCTEURS DE MATERIEL AEROSPATIAL Technopolis - 175, rue Jean-Jacques Rousseau - F-92138 Issy-les-Moulineaux Cedex - Tl. (1) 4

2、7.36.98.76 ICs : Descriptors : ENGLISH VERSION Aerospace series Cables, electrical, single and multicore for general purpose Operating temperatures between - 55 OC and 200 OC Part O10 : Screened (braided) and jacketed, YAG X3 laser printable Product standard Srie arospatiale Luft- und Raumfahrt Cble

3、s, lectriques, Leitungen, elektrisch, mono et multiconducteurs dusage gnral Tempratures de fonctionnement comprises entre - 55 OC et 200 OC Partie O10 : Blinds (tresss) et gains, ein- und mehradrig, fr allgemeine Verwendung Betriebstemperaturen zwischen -55 %und200 OC Teil O10 : Geschirmt (Umflechtu

4、ng) und ummantelt, marquables au laser YAG X3 Norme de produit YAG X3 Laser bedruckbar Produktnorm This “Aerospace Series“ Prestandard has been drawn up under the responsibility of AECMA (Association Europenne des Constructeurs de Matriel Arospatial). It is published on green paper for the needs of

5、AECMA-Members. It has been technically approved by the experts of the concerned Technical Committee following comment by the Member countries. Subsequent to the publication of this Prestandard, the technical content shall not be changed to an extent that interchangeability is affected, physically or

6、 functionally, without re-identification of the standard. After examination and signature of the AECMA Standard Checking Centre (NPS) and formal agreement of the Official Services of the Member countries it will be submitted as a draft European Standard to CE# (European Committee for Standardization

7、) for formal vote. Nota - Extra copies can be supDlied bv B.N.A.E. - Technoaolis 54 - 199, rue Jean-Jacauec Rousseau - 921 38 ISSY-LES-MOULINEAUX CEDEX I Comments should be sent within six months after the date of publication to I Edition approved for publication I AECMA I Technopolis - 1 75, rue Je

8、an-Jacques Rousseau 1995-03-31 C 2 Chairman M. Pezretta I 921 38 Issy-les-Moulineaux Cedex - FRANCE I Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-S

9、TD-AECMA PREN 2733-010-ENGL 1995 = L01233lI 0032799 733 Page 3 prEN 271 3-01 O : 1995 1 Scope This standard specifies the characteristics of YAG X3 laser printable, single and multicore screened (braided) and jacketed electrical cables for use in the on-board electrical systems of aircraft, at opera

10、ting temperatures between - 55 OC and 200 OC. It shall also be possible to mark these cables by hot stamp printing or ink jet printing. These markings shall be in accordance with EN 3838. 2 Normative references EN 2083 Copper and copper alloy conductors for electrical cables - Aerospace series EN 22

11、35 Aerospace series - Cables, electrical, single and multicore, screened and jacketed - Technical specification 2, EN 2266-003 Aerospace series - Cables, electrical, for general purpose - Operating temperatures between - 55 OC and 200 OC - Part 003 : Ink jet printable - Product standard 2, EN 2713-0

12、02 Aerospace series - Cables, electrical, single and multicore for general purpose - Operating temperatures between - 55 OC and 200 OC - Part 002 : Screened and jacketed - General 2, procedure General 2, electrical cables 2, EN 3042 Aerospace series - Quality assurance - EN aerospace products - Qual

13、ification EN 3475-100* Aerospace series - Cables, electrical, aircraft use - Test methods - Part 100 : EN 3838 Aerospace series - Requirements and tests on user-applied markings on aircraft 3 Definitions and symbols See EN 3475-100 4 Materials and construction 4.1 Materials These cables shall consis

14、t of the following : - cores according to EN 2266-003, top coat dispersion fluorocarbon; - number of cores 1 to 4. 2 to 4-core cables shall be twisted together according to EN 2235. Filler cores shall not be permitted. * 1) Published as AECMA Standard at the date of publication of this standard 2) P

15、ublished as AECMA Prestandard at the date of publication of this standard And all its parts quoted in table 2 Previous page is blank Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted

16、 without license from IHS-,-,-Page 4 prEN 271 3-01 O : 1995 Screening : - nickel-plated copper stranded braid; - for dimensions of strands, see table 1 ; - material according to EN 2083, tests according to EN 3475-100; - construction according to EN 2235. Outer jacket : - layer of polyimide with tot

17、al wall thickness (nominal value) of 30 ,um, coated on both sides with a layer 2,5 pm thick of fluorocarbon; - direction of winding immaterial - overlap 67 % min. ; or two layers - winding direction of first immaterial, overlap 51 % min. and second layer in opposite direction with 20 % min. overlap;

18、 - top coat of dispersion fluorocarbon, wall thickness 15 ,wn min. including the necessary additives for the acceptance of user-applied YAG X3 laser marking. 4.2 Construction See EN 2083 and table 1 Number sf cores Code for nominal section O0 1 002 004 006 o1 o o1 2 020 030 050 051 1 O0 1 002 004 00

19、6 o1 o o1 2 020 030 050 051 1 O0 1 002 004 006 o1 o o1 2 020 030 O0 1 002 004 006 o1 o o1 2 020 Nominal section mm2 0,15 0,25 0,4 0,6 1 12 2 3 5 5 Oll 5 0,25 O,4 0,6 1 If2 2 3 5 5 0,15 0,25 O,4 03 1 112 2 3 0,15 0,25 O,4 O, 6 1 12 2 Table 1 I Linear resistance 1 26 24 22 20 18 16 14 12 10 10 26 24 2

20、2 20 18 16 14 12 10 10 26 24 22 20 18 16 14 12 26 24 22 20 18 16 14 max. 160,O 114,O 60,O 33,2 21 ,I 14,5 10,9 618 4,2 4,1 165,OO 11 7,OO 61,70 34,l O 21,70 14,90 11,20 6,99 4,32 4,22 165,OO 11 7,OO 61,70 34,l O 21,70 14,90 11,20 6,99 165,O 11 7,O 61,7 34,l 21,7 14,9 11,2 Screen strands nominal diam

21、eter mm 0,08 0,08 0,lO 0,lO 0,IO 0,lO 0,IO 0,IO 0,12 0,12 0,IO 0,lO 0,IO 0,lO 0,lO Oll 2 0,12 0,15 0,15 0,15 0,lO 0,lO 0,lO 0,lO 0,12 0,12 0,12 0,15 0,lO 0,lO 0,IO 0,12 0,12 Oll 2 0.1 5 External diameter mm max. 1,50 1,60 1,82 2,07 2,32 2,58 2,85 3,40 4,10 4,25 2,41 2,59 2,91 3,41 3,95 4,55 5,09 6,1

22、6 7,60 7,70 2,53 2,73 3,08 3,64 4,25 4,84 5,40 6,66 2,74 2,97 3,35 4,05 4,66 5,28 6.10 Mass kglkm max. 5,8 618 9,1 12,9 17,1 22,1 27,7 40,8 64,4 66,6 10,6 12,5 15,9 22,8 31,6 43,4 55,8 85,2 126,7 132,0 13,5 16,2 21,4 31,7 46,0 61 ,I 77,6 122,8 16,1 19,8 26,4 41,6 57,5 76,2 103,0 1) Flexible construc

23、tion which may be used as an alternative 2) AWG = Closest American Wire Gage Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-EN 3475- 201 Test Details

24、Visual examination Applicable Flammability Applicable Extinguishing time : 3 s max. 408 409 Fire resistance Air-excluded ageing 502 Notch propagation Applicable Notch depth : 40 pm Page 5 prEN 2713-010 : 1995 4.3 See EN 271 3-002 Colour coding of cores and jacket 5 Required characteristics According

25、 to EN 2235 and EN 3475-100 See table 2 Mass Applicable ; see table 1 Applicable ; see table 1 Dimensions Electrical resistance per unit length Voltage proof test Insulation resistance Applicable ; see table 1 Applicable Applicable Applicable Not applicable I 304 Surface resistance I 305 Overload re

26、sistance I 401 Accelerated ageing Applicable Temperature (250 k 5) OC Shrinkage and delamination Appiica ble Temperature (250 i 5) OC Maximum shrinkage at each end of cable : jacket 2 mm, core insulation, see EN 2266-003 402 I 403 Delamination and blocking Applicable Temperature (250 k 5) OC Applica

27、ble Temperature (250 * 5) OC Maximum shrinkage at each end of cable : jacket 2 mm, core insulation, see EN 2266-003 Thermal shock 404 Bending at ambient temperature Applicable Cold bend test Applicable 407 Not applicable Not applicable Applicable 40 O00 h (temperature 200 OC) Applicable - 1 410 1 Th

28、ermal endurance I 41 1 I Resistance to fluids I 501 I Dynamic cut-through I Not aoplicable I Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-STD-AECMA

29、PREN 2713-010-ENGL 1995 m 10323LL 0032802 038 m EN 3475- I Test Page 6 prEN 271 3-01 O : 1995 Details Table 2 (concluded) Plating thickness Solderability Smoke density Applicable Not applicable Applicable 503 Resistance to wet arc tracking and electric arc propagation Resistance to dry arc tracking

30、and electric arc propagation Strippability and adherence of insulation to the conductor Braid screen pushback capability Permanence of manufacturers marking 504 Not applicable Not applicable Applicable Applicable Applicable Scrape abrasion Description block CABLE, ELECTRICAL Torsion Identity block E

31、N271 3-0 1 OB002F Tensile test on concentric 505 I conductors and strands I Number of this standard I r. Code letter for number of cores (see EN 2713-002, table 1) Applicable Test force on needle for cables 0,15 mm2 to 0,60 mm2 = 8 N 1,00 mm2 to 1,20 mm2 = 10 N 2,OO mm2 to 5,OO mm2 = 12 N Not aeelic

32、able Applicable 506 I Plating continuity I Applicable 507 I Adherence of elatinn 508 509 60 1 602 603 604 70 1 702 703 Toxicity I Applicable 6 Quality assurance See EN 3042 NOTE : If necessary, the code I9005 shall be placed between the description block and the identity block. Copyright Association

33、 Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,- STD-AECMA PREN 2713-OLO-ENGL 1995 M 1012311 0012803 T74 Page 7 prEN 2713-010 : 1995 8 Identification and marking See EN 271

34、 3-002 9 See EN 2235 Packaging, labelling and delivery lengths 1 O Technical specification See EN 2235 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-